• Title/Summary/Keyword: Engine cooling

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Transient Thermal Analysis on Wall Temperature Change of Rocket Engine Combustion Chamber Considering Film-Cooling (막냉각을 고려할 때 로켓엔진 연소실 벽면 온도변화에 대한 비정상 열해석)

  • Ha, Seong-Up;Lee, Seon-Mi;Moon, Il-Yoon;Lee, Soo-Yong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.5
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    • pp.37-46
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    • 2012
  • The calculation model for heat transfer analysis of rocket engine combustion chamber considering film-cooling has been established. Convective, radiative heat transfers and film-cooling effect in combustion chamber were evaluated using empirical equations especially for rocket engine combustors, and for heat transfer outward from chamber wall general convective and radiative equations were applied. Structural grid has been generated inside chamber wall for FVM calculations, and transient thermal analyses were carried out by time-marching techniques. LOx/kerosene rocket engine with chamber pressure of 50 bar has been analysed, and it is shown that, in that case, the film-cooling less than 4% remarkably contributes to reduce wall temperature, but the effect of the effect of film-cooling more than about 4% is not significantly increased.

Engine Room Layout Design Optimization of Fuel Cell Vehicle Using CFD Technique (CFD를 이용한 연료전지 차량 레이아웃 최적화)

  • Kim, Jung-Ill;Jeon, Wan-Ho;Cho, Jang-Hyung
    • Transactions of the Korean Society of Automotive Engineers
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    • v.19 no.4
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    • pp.99-106
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    • 2011
  • This paper deals with engine room layout design optimization of fuel cell electric vehicle (FCEV), which has been proposed as a potential alternative to fossil fuel depletion. Investing the great R&D efforts, the global vehicle manufacturers, especially Honda motor corporate, have shown not prototype vehicle but commercial vehicle using fuel cell in the market recently. In this paper, we analyze cooling performance and flow characteristic in the engine room of newly FCEV, in addition we suggest the optimization process for engine room layout design optimization. The two radiators in the vehicle for fuel cell stack and electronic components cooling have been analyzed and their performance are obtained in terms of cooling performance ratio (CPR). The value of CPR should always be less than one and based on criteria, we have achieved the optimum cooling performance of radiators for stack and electronic components. Aerodynamic performance is evaluated in terms of drag coefficient, improved through underbody modification using air devices.

NUMERICAL STUDY FOR COOLING CAPACITY IMPROVEMENT OF ENGINE ROOM ENCLOSURE SYSTEM (엔진실 차폐 시스템의 냉각성능 개선을 위한 수치적 연구)

  • Bae, Y.S.;Yoo, G.J.;Choi, H.K.
    • Journal of computational fluids engineering
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    • v.14 no.2
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    • pp.39-45
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    • 2009
  • In engine room, proper enclosure system is preferable for reducing noise level but the enclosure system in the engine room causes bad influence on cooling performance due to poor ventilation. Cooling efficiency of the enclosure system can be improved by varying fan speed and proper flow path for ventilation. In this study, numerical analysis is performed to assess cooling effect of the enclosure system using finite volume method. The RNG k-$\varepsilon$ model is adopted for turbulence model along with heat exchanger model and porous media model for heat exchanger analysis, and moving reference frame model for rotational fan. Verification result shows reasonable agreement with experimental data. Analysis results show direct effect of velocity and temperature distribution on cooling ability in the enclosure system. Enclosure system of case B shows high heat transfer coefficient and has the smallest area ratio of opened flow passages which is good for noise level reduction.

An Experimental Study on Engine Cooling System Improvement (엔진 냉각 시스템 개선에 관한 실험적 연구)

  • Chon, M.S.;Hwang, Y.H.
    • Journal of ILASS-Korea
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    • v.9 no.4
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    • pp.77-82
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    • 2004
  • This paper describes the improvement of engine cooling system. To improve engine cooling performance, the authors approached in two ways. One is to increase water pump performance, changing of impeller shape and lightening of material were carried out. The second one is cooling efficiency rise, which were investigated with head gasket coolant flow passage optimization with flow visualization technique. The test results show that water pump performance was increased effectively, reduction of pump drive torque, and increase of pump flow-rate and pressure rise. Gasket hole pattern optimization test results represent an optimized head coolant flow which stands cross flow from exhaust to intake port side and small vortex were removed.

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Analysis of fan clutch characteristics for electronic engine cooling control system (전자식 엔진냉각제어 시스템을 위한 팬 클러치 특성 분석)

  • Ryu, Hye-Yeon;Kim, Hyun-Hee;Jeong, Sung-Min;Koh, Young-Ho;Lee, Kyung-Chang
    • Journal of the Korean Society of Industry Convergence
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    • v.21 no.5
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    • pp.241-246
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    • 2018
  • The engine cooling system is a device that keeps the temperature of the engine room at a proper level by driving the cooling fan when the engine room temperature that occurs during driving is above a certain temperature. Recently, the vehicle cooling system has been changed to electronic system. Therefore, in this paper, we will analyze the clutch operation characteristics for designing a superior electronic fan clutch. For this purpose, an electronic fan clutch was designed and a test bed for performance evaluation was constructed and analyzed.

Circuit Capacity of Water Cooling on Domestic Small Diesel Engine (소형(小型)디젤 기관(機關)의 냉각수(冷却水) 순환량(循環量)에 대(對)한 연구(硏究))

  • Kim, Sung Rai;Myung, Byung Soo
    • Korean Journal of Agricultural Science
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    • v.19 no.1
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    • pp.91-96
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    • 1992
  • Diesel engine being used on power tiller has over heating problem while running at the rated power range, The reason for overheating the engine is mainly owing to so small capacity of cooling system. This study was conducted to determine relatively optimum capacity of cooling system for the diesel engine. The results obtained are summarized as follows. 1. The capacity of cooling system for the diesel engine being used in the rural area was not sufficient to cool the engine at the rated power. 2. It is desirable that the cooling water flow rate was $12{\ell}/min$ if we used supplementary pump for increasing the cooling efficiency. 3. As cooling water was circuited $12{\ell}/min$, highest temperature of cooling water was $91^{\circ}C$. This value is within $88^{\circ}C{\pm}5^{\circ}C$ of SAE Standard criterion.

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Thermal Analysis of Exhaust Diffuser Cooling Channels for High Altitude Test of Rocket Engine (로켓엔진 고공환경 모사용 디퓨져의 냉각 채널 열 해석)

  • Cho, Kie-Joo;Kim, Yong-Wook;Kan, Sun-Il;Oh, Seung-Hyub
    • Aerospace Engineering and Technology
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    • v.9 no.2
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    • pp.193-197
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    • 2010
  • Water cooling ducts are installed in the exhaust diffuser for high altitude tests of rocket engine to protect diffuser from high-temperature combustion gas. The mass flow rate and pressure of cooling water is designed to prevent boiling of cooling water in the ducts. Therefore, the estimation of maximum temperature of duct wall is important parameter in design of cooling system, especially pressure of cooling water. The method for predicting maximum temperatures of duct walls with variation of coolant flow rates was derived theoretically.

The Cooling Performance of Thrust Chamber with Film Cooling (막냉각에 따른 추력실의 냉각 성능)

  • Kim, Sun-Jin;Jeong, Hae-Seung
    • Journal of the Korea Institute of Military Science and Technology
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    • v.9 no.1 s.24
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    • pp.117-124
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    • 2006
  • Experiments on film cooling were performed with a small scale rocket engine homing liquid oxygen (LOx) and Jet A-1(jet engine fuel). Film coolants(Jet A-1 and water) were injected through the film cooling injector. Film cooled length and the outside wall temperature of the combustor were determined for chamber pressure, and the different geometries(injection angle) with the flow rates of film coolant. The loss of characteristic velocity due to film cooling was determined for the case of film cooling with water and Jet A-1. As the coolant flow increases, the outside wall temperatures decrease but the decrease in the outside wall temperatures reduced over the 8 percent film coolant flow rate. The efficiency of characteristic velocity was decreased with the Increase of the film coolant flow rate.

Evaluation of Heat Balance for Cooling System of an Armored Installation in Small Space (좁은 공간 내의 밀폐형 장치 냉각시스템에 대한 열평형 평가)

  • Kim, Sung-Kwang;Ahn, Seok-Hwan;Nam, Ki-Woo
    • Journal of Ocean Engineering and Technology
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    • v.21 no.3 s.76
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    • pp.1-7
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    • 2007
  • In this study, the heat balance test of an engine was conducted, and the heat released to coolant is measured and corrected using a power adjustment factor for high fuel temperature to simulate heat rejection of the engine. An engine-converter matching simulation program which can compute the engine speed, transmission output speed, transmission input and output power is developed from the vehicle, transmission and engine performance curve. With this information and the engine heat rejection characteristics, the engine and transmission heat rejection rates can be determined at given condition. In analyzing the air mass flow, a sub program computing the air mass flow rate from the equation of the pressure balance between cooling fan static pressure rise and pressure losses of cooling components is developed.

Numerical analysis for development of vehicle engine room cooling hood (차량 엔진룸 냉각용 후드 개발을 위한 수치해석)

  • Lee, Suk Young
    • Journal of Energy Engineering
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    • v.27 no.4
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    • pp.92-97
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    • 2018
  • This study deals with the numerical analysis for hood development to improve the cooling effect of the engine related components in engine room. Reducing the component temperature in engine room caused by a sudden temperature deviation can minimize the durability degradation of components. Therefore, in this study, numerical analysis for the development of the hood in engine room was carried out in four parts such as generator, battery, ECU and power steel oil which are relatively easy to control temperature among the main components in engine room. In order to verify the numerical analysis, experiments were conducted under the same conditions as those assumed in the numerical analysis.